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Application of the compressible and low-mach number approaches to large-eddy simulation of turbulent flows in aero-engines

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Academic year: 2021

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Figure

Figure 1.1: Development of the worldwide transported flight passengers. Source: ICAO / Airbus
Figure 4.6: Order of accuracy in time of TRK4 for varying values of the parameter α.
Figure 4.9: Mean resolved kinetic energy decrease in DNS and LES with TRK4 for two values of the parameter α.
Figure 5.1: Evolution of the vortex for AVBP (TTGC, C = 0.7) at di erent instances illustrated for the induced stream wise velocity u U 0 .
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